JPS62197696A - Cooling turbofan for engine - Google Patents

Cooling turbofan for engine

Info

Publication number
JPS62197696A
JPS62197696A JP3965986A JP3965986A JPS62197696A JP S62197696 A JPS62197696 A JP S62197696A JP 3965986 A JP3965986 A JP 3965986A JP 3965986 A JP3965986 A JP 3965986A JP S62197696 A JPS62197696 A JP S62197696A
Authority
JP
Japan
Prior art keywords
blade
fan
engine
rotor
turbofan
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP3965986A
Other languages
Japanese (ja)
Other versions
JPH0765595B2 (en
Inventor
Yasuo Terada
保男 寺田
Yoshiyuki Matsuda
佳之 松田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honda Motor Co Ltd
Original Assignee
Honda Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to JP61039659A priority Critical patent/JPH0765595B2/en
Publication of JPS62197696A publication Critical patent/JPS62197696A/en
Publication of JPH0765595B2 publication Critical patent/JPH0765595B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To reduce noise by installing an annular straightening plate in concentric form to a turbofan onto the front edge surface of each blade of the turbofan fixed at the top edge part of a rotor. CONSTITUTION:The rotor 4 of an AC generator 3 is installed at the top edge part of the crankshaft 2 of an engine 1, and a turbofan 5 is fixed at the top edge part of the rotor 4. An annular straightening plate 11 in common for each blade is installed in concentric form to the turbofan 5 at the front edge surface of each blade 10 of the fan 5. Therefore, the air stream is straightened in the centrifugal direction, and no eddy current is generated between the front edge surface of a blade and a shroud, and noise is reduced.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、エンジンの冷却ターボファンに係り、特に騒
音が小さく冷却効率のよい冷却ターボファンに係る。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to an engine cooling turbo fan, and particularly to a cooling turbo fan with low noise and high cooling efficiency.

〔従来の技術〕[Conventional technology]

従来例えば自動2輪車のエンジンの回りを冷却する冷却
ファンとしては、エンジンのクランク軸によって回転す
る交流発電機のロータ外面に付設されており、軸流型と
遠心型とが利用される。
Conventionally, cooling fans for cooling the engine of a two-wheeled motor vehicle, for example, are attached to the outer surface of the rotor of an alternator that is rotated by the crankshaft of the engine, and axial flow type and centrifugal type are used.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

一般に遠心型(ターボファン)は全厚が低いために騒音
の低減に有利であるが、送風流量を同径の軸流型ファン
(出口角90”以上)と同じ流量を得るためには、ファ
ンの厚み(高さ)を増加させなければならないため、ス
ペースの小さいスクータには不向であった。
In general, centrifugal fans (turbo fans) are advantageous in reducing noise due to their low overall thickness, but in order to obtain the same flow rate as an axial flow fan with the same diameter (exit angle of 90” or more), the fan This required an increase in the thickness (height) of the motor, making it unsuitable for scooters with small spaces.

ところで、ファンの高さDと送風流iQとの関係は第4
図に示すように、理論的にはQ−Dであるが、スクータ
クラス(φ200 mm以下)のファンでは高さDに対
して流量Qは低下気味となる。
By the way, the relationship between the fan height D and the air flow iQ is the fourth
As shown in the figure, although theoretically it is Q-D, the flow rate Q tends to decrease with respect to the height D in a scooter class (φ200 mm or less) fan.

その理由は第6図に示すようにファン前面に配設したシ
ュラウドとの間に逆流が生じ、抵抗が大きくなるためと
考えられる。
The reason for this is thought to be that, as shown in FIG. 6, a backflow occurs between the fan and the shroud disposed in front of the fan, increasing resistance.

〔問題点を解決するための手段〕[Means for solving problems]

本発明は前記のような問題点を解決しスクータのような
設置スペースの小さな車両に適した小型で送風及び冷却
効率が高く、騒音の低いエンジン用冷却ターボファンを
提供することを目的として開発したもので、具体的な手
段としては、エンジンにより駆動される発電機のロータ
先端部にターボッアンを固定すると共に、環状の整流板
を各ブレード前端面にターボファンと同心状に装設した
エンジンの冷却ターボファンを構成するものである。
The present invention was developed with the aim of solving the above-mentioned problems and providing an engine cooling turbo fan that is compact, has high air blowing and cooling efficiency, and has low noise, suitable for vehicles with small installation spaces such as scooters. Specifically, a turbo fan is fixed to the tip of the rotor of a generator driven by the engine, and an annular rectifier plate is installed on the front end of each blade concentrically with the turbo fan to cool the engine. This constitutes a turbo fan.

〔作 用〕[For production]

ターボファンはロータの回転と共に回転して発電機回り
及びエンジン回りを冷却する。ターボファンのブレード
はファンの回転軸心から放射方向に設けられているが、
そのブレードの軸方向前端面に環状整流板が付設されて
いるため、気流は整流板の中央孔からファンの回転軸方
向へ流動し、各ブレードによって遠心方向へ飛ばされる
。このとき、整流板は遠心方向へ流動する風流を出口方
向へ整流するため、ファンによって引き込んだ風流の一
部が逆流することはなく、整流板面を摺動する風流は速
度を早めるので、送風流量を増加させる作用がある。
The turbo fan rotates with the rotation of the rotor to cool the area around the generator and engine. The blades of a turbo fan are installed in a radial direction from the rotation axis of the fan.
Since an annular baffle plate is attached to the front end surface of the blade in the axial direction, the airflow flows from the central hole of the baffle plate in the direction of the rotation axis of the fan, and is blown in the centrifugal direction by each blade. At this time, the rectifying plate rectifies the airflow flowing in the centrifugal direction toward the outlet, so a part of the airflow drawn in by the fan does not flow backwards, and the speed of the airflow sliding on the rectifying plate surface increases, so the airflow is It has the effect of increasing the flow rate.

送風流量が増加する分だけブレードの高さを低くするこ
とが可能となり、ファン全体を小型化させられるので、
スクータ等のようにスペースの小さい車種にも騒音低下
のできるターボファンを搭載することができる。
The height of the blades can be lowered by the amount of air flow that increases, making the entire fan smaller.
Turbo fans that can reduce noise can be installed even in small space vehicles such as scooters.

〔実施例〕〔Example〕

本発明の実施例を図面に基づいて説明する。第1図はエ
ンジンに装着された交流発電機と冷却ターボファンの関
係を示す断面図である。
Embodiments of the present invention will be described based on the drawings. FIG. 1 is a sectional view showing the relationship between an alternator installed in an engine and a cooling turbo fan.

車両のエンジン1のクランク軸2先端部には交流発電機
3のロータ4が装着されており、ロータ4の軸2方向先
端面にターボファン5がロータ4と同心状に装着され、
ボルト6で固定されている。
A rotor 4 of an alternator 3 is attached to the tip of the crankshaft 2 of the engine 1 of the vehicle, and a turbo fan 5 is attached to the tip of the rotor 4 in the axial direction 2 concentrically with the rotor 4.
It is fixed with bolt 6.

ターボファン5の軸2方向先端部前方には、発電機3及
びターボファン5をカバーするようにシュラウド7が設
けられ、その吸気ロアAはターボファン5と同心状に位
置して開設されている。
A shroud 7 is provided in front of the tip of the turbofan 5 in the axial direction 2 to cover the generator 3 and the turbofan 5, and its intake lower A is located concentrically with the turbofan 5. .

前記ターボファン5は第2図及び第3図に示すように、
基体8は平面円形で、中央部を山状に高く膨出させた膨
出部9を形成すると共に、基体8周縁部には、放射方向
における均等間隔配列をもって複数のブレード10.1
0・・・を遠心方向へ張り出し、かつ回転方向(右)に
対して逆回りの低油状に形成して出口角θは90度より
小さく形成しである。
The turbo fan 5, as shown in FIGS. 2 and 3,
The base body 8 has a circular planar shape, and has a bulge portion 9 that bulges out in the shape of a mountain at the center, and a plurality of blades 10.1 arranged at equal intervals in the radial direction on the periphery of the base body 8.
0... is formed in a low oil shape that extends in the centrifugal direction and rotates in the opposite direction to the rotation direction (right), and the exit angle θ is formed to be smaller than 90 degrees.

各ブレード10.10・・・の前端面ば回転軸心線りに
対して後方へ傾斜するテーパ状に形成し、該各ブレード
10.10前端面には各ブレード共通の環状整流板11
をターボファン5と同心状に装着しである。
The front end surface of each blade 10.10... is formed in a tapered shape that slopes backward with respect to the rotation axis, and the front end surface of each blade 10.10 has an annular rectifying plate 11 common to each blade.
is installed concentrically with the turbo fan 5.

また各ブレード10.10の後端面には環状支持体12
を回転軸心線りと同心状に固着しである。
Also, on the rear end surface of each blade 10.10 is an annular support 12.
It is fixed concentrically with the rotation axis.

前記基体8前面にはボルト孔8Aを有する固定部8Bを
形成してあり、その位置はロータ4の固定ネジ孔4Aと
同じ配置としてあり、ボルト6をボルト孔8Aに挿通さ
せ固定ネジ孔4Aに螺合させることでターボファン5を
ロータ4に固定させる。
A fixing part 8B having a bolt hole 8A is formed on the front surface of the base body 8, and its position is the same as the fixing screw hole 4A of the rotor 4. A bolt 6 is inserted into the bolt hole 8A and inserted into the fixing screw hole 4A. The turbo fan 5 is fixed to the rotor 4 by screwing together.

これらターボファン5は、基体8.ブレード10、環状
整流板11.支持体12ともプラスチックで一体成形に
より製作する。
These turbo fans 5 have a base 8. Blade 10, annular current plate 11. The support body 12 is also made of plastic and manufactured by integral molding.

以上の構成により成る本発明において、ロータ4の回転
に伴い同時にターボファン5が矢示方向へ回転すると、
吸気ロアAからダクト7B、7Bを通って吸入された外
気は、膨出部9の傾斜面を遠心方向へ流動してブレード
10.10によって遠心力で遠心方向へ圧送される。こ
の過程において、各ブレード10.10前端部における
気流は環状整流板11に摺接してブレード後方に押され
てエンジン1方向へ整流されると共に、流速を早めて流
量が増加するため冷却効果を高める。すなわち第4図に
示すように、従来型と本発明ファンPとを比較すると、
ブレードの高さDに対して流11Qは本発明の方が大き
くなり、その結果、従来型と同じ径で同じ流量を得るた
めには、hだけ低くしてもよいことになり、すなわち、
そのh分だけブレードを低く、ファン全体を小型化する
ことが可能となる。
In the present invention having the above configuration, when the turbo fan 5 simultaneously rotates in the direction of the arrow as the rotor 4 rotates,
The outside air taken in from the intake lower A through the ducts 7B, 7B flows in the centrifugal direction on the inclined surface of the bulging portion 9, and is forced in the centrifugal direction by the centrifugal force by the blades 10.10. In this process, the airflow at the front end of each blade 10.10 slides into contact with the annular rectifying plate 11, is pushed toward the rear of the blade, and is rectified in the direction of the engine 1, increasing the flow velocity and increasing the flow rate, thereby enhancing the cooling effect. . That is, as shown in FIG. 4, when comparing the conventional type and the fan P of the present invention,
The flow 11Q of the present invention is larger with respect to the blade height D, and as a result, in order to obtain the same flow rate with the same diameter as the conventional type, it can be lowered by h, that is,
The blades can be lowered by that amount h, making it possible to downsize the entire fan.

また環状整流板11があるためにブレード10の前端面
とシュラウド7との間においで渦流が生じなくなり、第
5図に示すグラフのように、従来型ファンに比較して著
しく音圧レベルを低下させることができて低騒音ファン
を提供することができる。
In addition, because of the annular current plate 11, no vortex is generated between the front end surface of the blade 10 and the shroud 7, and as shown in the graph shown in FIG. 5, the sound pressure level is significantly reduced compared to the conventional fan. It can provide a low noise fan.

本発明は前記構成に限定されるものではなく、適宜設計
変更することができる。
The present invention is not limited to the above configuration, and the design can be changed as appropriate.

〔発明の効果〕〔Effect of the invention〕

本発明は次のようなすぐれた効果を有している。 The present invention has the following excellent effects.

A、各ブレードの前端面に環状整流板が設けられている
ため、気流が遠心方向へ整流されて、ブレード前端面と
シュラウド間に渦流が生じず、騒音が低下され、かつ送
風流速が早まり、流量が増加して冷却効果が向上する。
A. Since an annular rectifying plate is provided on the front end surface of each blade, the airflow is rectified in the centrifugal direction, no vortex is generated between the blade front end surface and the shroud, noise is reduced, and the air flow speed is increased. The flow rate increases and the cooling effect improves.

B、流量の増加に伴い、増加した分だけ従来型ファンよ
りもブレードの高さを低く或いは径を小さくすることが
できるため、ファン全体の小型化が可能となり、スペー
スの小さなスクータ等に低騒音ターボファンを搭載する
ことができる。
B. As the flow rate increases, the height of the blades can be made lower or the diameter smaller than that of conventional fans, making it possible to downsize the entire fan and provide low noise for small space scooters etc. Can be equipped with a turbo fan.

【図面の簡単な説明】[Brief explanation of drawings]

図面は本発明に係り、第1図は交流発電機のロータに装
設されたターボファンの断面図、第2図はターボファン
の一部正面図、第3図はターボファンの断面図、第4図
はブレードの高さと風量の関係を示すグラフ、第5図は
ファン回転速度と音圧レベルの関係を示すグラフ、第6
図は従来型ターボファンの断面図。 1・・・エンジン     2・・・クランク軸3・・
・交流発電機    4・・・ロータ5・・・ターボフ
ァン   7・・・シュラウド7A・・・吸気口   
  7B・・・ダクト8・・・基 体      8A
・・・ボルト孔8B・・・固定部     9・・・膨
出部10・・・ブレード     11・・・環状整流
板12・・・環状支持体 特許出願人  本田技研工業株式会社 り一
The drawings relate to the present invention; FIG. 1 is a sectional view of a turbo fan installed in the rotor of an alternator, FIG. 2 is a partial front view of the turbo fan, FIG. 3 is a sectional view of the turbo fan, and FIG. Figure 4 is a graph showing the relationship between blade height and air volume, Figure 5 is a graph showing the relationship between fan rotation speed and sound pressure level, and Figure 6 is a graph showing the relationship between fan rotation speed and sound pressure level.
The figure is a cross-sectional view of a conventional turbo fan. 1...Engine 2...Crankshaft 3...
・AC generator 4...Rotor 5...Turbo fan 7...Shroud 7A...Intake port
7B...Duct 8...Base 8A
...Bolt hole 8B...Fixing part 9...Bulging part 10...Blade 11...Annular current plate 12...Annular support patent applicant Riichi Honda Motor Co., Ltd.

Claims (1)

【特許請求の範囲】[Claims] エンジンにより駆動される発電機のロータ先端部にター
ボファンを同心状に固定する共に、環状整流板を各ブレ
ード前端面にターボファンの回転軸心と同心状に装設し
たことを特徴とするエンジンの冷却ターボファン。
An engine characterized in that a turbo fan is fixed concentrically to the tip of a rotor of a generator driven by the engine, and an annular baffle plate is installed on the front end surface of each blade concentrically with the rotation axis of the turbo fan. cooling turbo fan.
JP61039659A 1986-02-25 1986-02-25 Engine cooling turbine Expired - Fee Related JPH0765595B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61039659A JPH0765595B2 (en) 1986-02-25 1986-02-25 Engine cooling turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61039659A JPH0765595B2 (en) 1986-02-25 1986-02-25 Engine cooling turbine

Publications (2)

Publication Number Publication Date
JPS62197696A true JPS62197696A (en) 1987-09-01
JPH0765595B2 JPH0765595B2 (en) 1995-07-19

Family

ID=12559211

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61039659A Expired - Fee Related JPH0765595B2 (en) 1986-02-25 1986-02-25 Engine cooling turbine

Country Status (1)

Country Link
JP (1) JPH0765595B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8151935B2 (en) 2005-02-21 2012-04-10 Geoff Graham Lifting and positioning apparatus
JP2014101888A (en) * 2006-05-24 2014-06-05 Resmed Motor Technologies Inc Compact low noise efficient blower for cpap devices
CN109790850A (en) * 2016-09-30 2019-05-21 本田技研工业株式会社 The cooling fan of internal combustion engine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5037044U (en) * 1973-07-31 1975-04-18
US4350123A (en) * 1980-02-09 1982-09-21 Solo Kleinmotoren Gmbh Hand-held power tool with a combustion motor
JPS59182698U (en) * 1983-05-25 1984-12-05 カルソニックカンセイ株式会社 Synthetic resin Sirotskov fan
JPS60185042U (en) * 1984-05-19 1985-12-07 本田技研工業株式会社 forced air cooled engine
JPS6140495A (en) * 1984-07-31 1986-02-26 Matsushita Electric Ind Co Ltd Electric blower

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5037044U (en) * 1973-07-31 1975-04-18
US4350123A (en) * 1980-02-09 1982-09-21 Solo Kleinmotoren Gmbh Hand-held power tool with a combustion motor
JPS59182698U (en) * 1983-05-25 1984-12-05 カルソニックカンセイ株式会社 Synthetic resin Sirotskov fan
JPS60185042U (en) * 1984-05-19 1985-12-07 本田技研工業株式会社 forced air cooled engine
JPS6140495A (en) * 1984-07-31 1986-02-26 Matsushita Electric Ind Co Ltd Electric blower

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8151935B2 (en) 2005-02-21 2012-04-10 Geoff Graham Lifting and positioning apparatus
JP2014101888A (en) * 2006-05-24 2014-06-05 Resmed Motor Technologies Inc Compact low noise efficient blower for cpap devices
US9677563B2 (en) 2006-05-24 2017-06-13 Resmed Motor Technologies Inc. Compact low noise efficient blower for CPAP devices
US10605246B2 (en) 2006-05-24 2020-03-31 Resmed Motor Technologies Inc. Compact low noise efficient blower for CPAP devices
US11353030B2 (en) 2006-05-24 2022-06-07 Resmed Motor Technologies Inc. Compact low noise efficient blower for CPAP devices
US11892000B2 (en) 2006-05-24 2024-02-06 Resmed Motor Technologies Inc. Compact low noise efficient blower for CPAP devices
CN109790850A (en) * 2016-09-30 2019-05-21 本田技研工业株式会社 The cooling fan of internal combustion engine
CN109790850B (en) * 2016-09-30 2020-10-30 本田技研工业株式会社 Cooling fan for internal combustion engine

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